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[texts]Scale and turbulence effects on the lift and drag characteristics of the NACA 653-418, a = 1.0 airfoil section - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003605349&ix=nu&I=0&V=D&pm=1
Keywords: Reynolds number; Aerofoils; Aerodynamics--Research
Downloads: 129
[texts]Scale-effect tests in a turbulent tunnel of the NACA 653-418, a = 1.0 airfoil section with 0.20-airfoil-chord split flap - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003613066&ix=nu&I=0&V=D&pm=1
Keywords: Reynolds number; Aerofoils; Aerodynamics--Research
Downloads: 75
[texts]Simple method for estimating terminal velocity including effect of compressibility on drag - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003638273&ix=nu&I=0&V=D&pm=1
Keywords: Compressibility; Aerodynamics--Research
Downloads: 86
[texts]Simple numerical method for the calculation of the laminar boundary layer - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003779544&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Laminar boundary layer
Downloads: 87
[texts]Solution of the laminar-boundary-layer equation for the flat plate for velocity and temperature fields for variable physical properties and for the diffusion field at high concentration : = Über die lösung der laminaren grenzschichtgleichung an der ebenen platte für geschwindigkeits- und temperaturfeld bei veränderlichen stoffwerten und für das diffusionsfeld bei höheren konzentrationen - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003689761&ix=nu&I=0&V=D&pm=1
Keywords: Boundary layer; Laminar flow
Downloads: 119
[texts]Some effects of heat transfer at Mach number 2.0 at stagnation temperatures between 2,310° and 3,500° R on a magnesium fin with several leading-edge modifications - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003853254&ix=nu&I=0&V=D&pm=1
Keywords: Heat--Transmission; Aerodynamics--Research; Magnesium--Electrometallurgy
Downloads: 97
[texts]Some examples of the applications of the transonic and supersonic area rules to the prediction of wave drag - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003809079&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics, Transonic; Aerodynamics, Supersonic; Aerodynamics--Research
Downloads: 181
[texts]Some experiences regarding the nonlinearity of hot wires - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003760215&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Heat--Transmission
Downloads: 59
[texts]Some measurements of time and space correlation in wind tunnel - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003807829&ix=nu&I=0&V=D&pm=1
Keywords: Turbulence--Research; Aerodynamics--Research
Downloads: 98
[texts]Some notes on the determination of the stick-free neutral point from wind-tunnel data - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003804989&ix=nu&I=0&V=D&pm=1
Keywords: Elevators (Airplanes; Aerodynamics--Research
Downloads: 91
[texts]Spinning of large airplanes - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003613597&ix=nu&I=0&V=D&pm=1
Keywords: Bombers; Transport planes; Aerodynamics--Research
Downloads: 136
[texts]Stability in a body stabilized by fins and suspended from an airplane - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003617553&ix=nu&I=0&V=D&pm=1
Keywords: Air-speed indicators; Aerodynamics--Research
Downloads: 79
[texts]Static-pressure error of an airspeed installation on an airplane in high-speed dives and pull-outs - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003616343&ix=nu&I=0&V=D&pm=1
Keywords: Static pressure probes; Aerodynamics--Research
Downloads: 72
[texts]Steady vibrations of wing of circular plan form, and, theory of wing of circular plan form - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003779524&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Airplanes--Wings--Testing
Downloads: 167
[texts]Stresses around rectangular cut-outs in skin-stringer panels under axial loads - II - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003806425&ix=nu&I=0&V=D&pm=1
Keywords: Strains and stresses; Aerodynamics--Research
Downloads: 99
[texts]Study of the effects of radii of gyration and altitude on aileron effectiveness at high speed - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003805033&ix=nu&I=0&V=D&pm=1
Keywords: Ailerons; Aerodynamics--Research
Downloads: 116
[texts]Study of the flow over a 45° sweptback wing -fuselage combination at transonic Mach numbers - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003809146&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics, Transonic; Airplanes--Wings, Swept-back; Aerodynamics--Research
Downloads: 71
[texts]Summary of available knowledge concerning skin friction and heat transfer and its application to the design of high-speed missiles - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003810325&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics--Research; Skin friction (Aerodynamics
Downloads: 238
[texts]Summary of information on support interference at transonic and supersonic speeds - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003808466&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics, Transonic; Aerodynamics, Supersonic
Downloads: 112
[texts]Supersaturation in the spontaneous formation of nuclei in water vapor - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003807868&ix=nu&I=0&V=D&pm=1
Keywords: Condensation--Research; Aerodynamics--Research
Downloads: 65
[texts]Supersonic-tunnel tests of projectiles in Germany and Italy - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003598987&ix=nu&I=0&V=D&pm=1
Keywords: Mach number; Projectiles, Aerial; Aerodynamics--Research
Downloads: 107
[texts]Survey of advantages and problems associated with transpiration cooling and film cooling of gas-turbine blades - Lewis Research Center
http://uf.catalog.fcla.edu/uf.jsp?st=UF003810653&ix=nu&I=0&V=D&pm=1
Keywords: Turbines--Blades--Research; Airplanes--Motors--Cooling; Aerodynamics--Research
Downloads: 80
[texts]Systematic investigations of the influence of the shape of the profile upon the position of the transition point - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003875302&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Boundary layer--Research
Downloads: 138
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